Preview Questions Aircraft Maintenance Technician | Role Specific Skill

Question 1: What role does "Magnetic Particle Inspection" (MPI) play in aircraft structural inspections, and what does it primarily detect?

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It is used to detect corrosion in the aircraft's fuselage

It helps detect electrical malfunctions in the control systems

It is used to detect surface and subsurface cracks in ferromagnetic materials

It is used to inspect the exhaust system for leaks

Question 2: What is the most common troubleshooting step for resolving abnormal vibrations felt through the flight control yoke?

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Check the balance of the aircraft's propeller

Inspect control cables for looseness

Examine the flight control servos for wear

Inspect the main landing gear struts for damage

Question 3: What could be the cause of low engine performance if an aircraft experiences reduced thrust during takeoff?

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Potential issues with the engine's air intake system, fuel delivery, or compressor stages

A problem with the aircraft's wheel alignment

A malfunction in the aircraft's hydraulic system

An issue with the avionics system, affecting the engine control

Question 4: During routine maintenance, what is the purpose of an engine "ground run-up" test?

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To ensure proper idle speed and RPM control

To verify the proper functioning of the engine's power turbine

To test the engine's fuel efficiency

To ensure engine thrust levels meet specifications

Question 5: In the repair of an aircraft wing's spars, what is the most important consideration regarding the alignment of the wing?

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Ensuring the spars are aligned to distribute loads evenly

Ensuring the spars are aligned to maintain the wing's aerodynamic shape

Ensuring the spars are positioned to minimize weight

Ensuring the spars are aligned to match the fuselage

Question 6: In a thorough inspection of an aircraft's wing, what would be the most likely cause of a failure if there is evidence of deformation around the wing's attachment points?

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Faulty hydraulic actuation system causing pressure buildup

Excessive fuel weight in the wing

Fatigue cracks caused by repeated stress

Improper installation of the wing to the fuselage